Model of structure of re-entry vehicle mounted on multistage rocket booster is constructed; dynamic environment to which it is subjected during ballistic flight is considered as to source and character of forces involved; dynamic model of system is presented and equations of motion written; dynamic model of re-entry vehicle-shaker combination is presented; results show that simulation of shear and slope at interface of vehicle during vibration test by proper fixture design is feasible using methods and approximations included in report.
Simulation of in-flight lateral bending modes for electrodynamic shaker testing
AIAA -- Tech Paper
Meeting of the AIAA -- Simulation for Aerospace Flight Conference ; 1963 Re-entry
1963
10 pages
Aufsatz (Konferenz)
Englisch
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